# N913FD: Boeing 757-28A - Status: Valid registration - Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 seats) - Serial number: 24017 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: November 4, 2008 - Expires: November 30, 2028 - Mode S code: ACA251 - Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913FD - Page: https://openairdocs.org/aircraft/N913FD From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Boeing 757-28A) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N913FD. ## FAA accident and incident reports None matched to N913FD. ## Service difficulty reports (184, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA202504020553](https://openairdocs.org/sdr/FDEA202504020553), Apr 2, 2025: FLOOR SUPPORT. MISALIGNED. STA. 580 TO 600 LBL 45.5 BLOW OUT PANEL STRUCTURE IS MISSALIGNED. ACCOMPLISHED WITH EA# F5330-T0382716 P1, TITLE "FUSELAGE-FLOOR BEAMS REPAIR OF MISALIGNED FAST - [SDR FDEA202504020552](https://openairdocs.org/sdr/FDEA202504020552), Apr 2, 2025: FRAME. DAMAGED. CABIN R/H FRAME HAS A FASTENER SHEARED AND THE HOLE IS ELONGATED AT STA 1640, BETWEEN STR 8R-9R DOT# 3521. ACCOMPLISHED REPAIR ON EA# F-5310-T0382395 P1 "FUSELA - [SDR FDEA202503290537](https://openairdocs.org/sdr/FDEA202503290537), Mar 29, 2025: SKIN. NOT REPORTED. WHILE ACCOMPLISHING GVI OF STRINER S-14L LAP SPLICE ON EO F-5330-E0344603 P1 STEP 3.A A SKIN REPAIR DOUBLER WAS FOUND INSTALLED AT STA. 1600-STA 1620 STRINGER S - [SDR FDEA202503280530](https://openairdocs.org/sdr/FDEA202503280530), Mar 28, 2025: SKIN. CORRODED. (DOT 38-24) RH LOWER FUSELAGE SKIN CORRODED STA 1788 APPROX 4" AREA, 3" ABOVE THE APU RH DOOR CUTOUT. COMPLIED WITH REPAIR ON EA F-5330-T0382463 P1 FUSELAGE-PLA - [SDR FDEA202503240484](https://openairdocs.org/sdr/FDEA202503240484), Mar 24, 2025: SEAT TRACK. CORRODED. MCD SEAT TRACK RBL 47.5 I/B FLANGE HAS CORROSION AT STA. 1460 AND 1520 REMOVED AND REPLACED DAMAGE SEAT TRACK FROM BS 1420 TO BS 1520 AT RBL 47.5 ON MATERIAL P/ - [SDR FDEA202503220474](https://openairdocs.org/sdr/FDEA202503220474), Mar 22, 2025: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 58.22 HAS CORROSION AT STA 1108, 1140, 1170, AND 1180- DOT 45-048 REMOVED AND REPLACED SEAT TRACK AT MAIN DECK, FROM STA 900 TO STA 1180 IAW S - [SDR FDEA202503200464](https://openairdocs.org/sdr/FDEA202503200464), Mar 20, 2025: STRAP. CORRODED. DOT 80-021 AFT CARGO COMPARTMENT F/S 1380-1460 CEILING AREA RH SIDE FLOOR BEAM STABILIZATION STRAP CORRODED. REMOVED AND REPLACED STABILIZATION STRAP AFT CARGO - [SDR FDEA202503150428](https://openairdocs.org/sdr/FDEA202503150428), Mar 15, 2025: FLOOR PANEL. DELAMINATED. (DOT 38-31) MDC FLOOR PANEL 252MTF DELAMINATED BS1620-1640 RBL58.22 FABRICATED FLOOR PANEL 252 MTF ZONE 250 ON VTMAE TRAVELER #T25/1804424 IAW MAE DWG PL1186418 - [SDR FDEA202503150427](https://openairdocs.org/sdr/FDEA202503150427), Mar 15, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL 232 MJF DAMAGED FABRICATED FLOOR PANEL 232 MJF ZONE 230 ON VTMAE TRAVELER #T25/1802791 IAW MAE DWG 11862181 REV. L MAJOR REPAIR - [SDR FDEA202503150426](https://openairdocs.org/sdr/FDEA202503150426), Mar 15, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL 252 MSF DAMAGED FABRICATED FLOOR PANEL 252 MSF ZONE 250 ON VTMAE TRAVELER #T25/1802794 IAW MAE DWG PL 11864182 MAJOR REPAIR - [SDR FDEA202503140416](https://openairdocs.org/sdr/FDEA202503140416), Mar 14, 2025: FLOOR PANEL. DAMAGED. FLOORBOARD 242MHF AT STA 1019 RBL 64.2 HAS INSERT PULLED OUT WITH SCREW STILL IN THE FLOOR STRUCTURE- DOT 45-045 FABRICATED FLOOR PANEL 242MHF ZONE 240 ON VTMAE - [SDR FDEA202503140415](https://openairdocs.org/sdr/FDEA202503140415), Mar 14, 2025: FLOOR PANEL. DAMAGED. FLOORBOARD PANEL 242MAF HAS INSERT PULLED OUT AND FASTENER STILL IN FLOOR STRUCTURE- DOT 45-048 FABRICATED FLOOR PANEL 242MAF ZONE 240 ON VTMAE TRAVELER #T25/18 - [SDR FDEA202503140414](https://openairdocs.org/sdr/FDEA202503140414), Mar 14, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL 222 BF DAMAGED FABRICATED FLOOR PANEL 222BF ZONE 220 ON VTMAE TRAVLER #T25/1802961 IAW BOEING DWG PL141N5361 REV. BC, MAJOR REPAIR - [SDR FDEA202503140413](https://openairdocs.org/sdr/FDEA202503140413), Mar 14, 2025: FLOOR PANEL. DAMAGED. FLOORBOARD PANEL 241MPF HAS PULLED INSERT- DOT 45-052 FABRICATED FLOOR PANEL 241MPF ZONE 240 ON VTMAE TRAVELER #T25/1802792 IAW MAE DWG PL11863182, MAJOR REPAIR - [SDR FDEA202412131800](https://openairdocs.org/sdr/FDEA202412131800), Dec 13, 2024: WARNING MESSAGE. FALSE ACTIVATION. ON FINAL (RWY 27 KMEM) 170 KIAS 1200AGL, FLAPS 20 TO 25, GEAR DOWN GOT TE FLAP DISAGREE EICAS. EXECUTED GO AROUND, RAN QRH, LANDED WITHOUT INCIDENT EMERGENCY DE - [SDR FDEA202304170800](https://openairdocs.org/sdr/FDEA202304170800), Apr 17, 2023: FLOORBEAM. CRACKED. FOUND CRACK ON FLOOR BEAM AT STA 580 AT LBL 45 ON UPPER FLANGE LOWER AREA WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A# F-5310-T0374058-FLOOR BEAM AT STA 580 - [SDR FDEA202304160703](https://openairdocs.org/sdr/FDEA202304160703), Apr 16, 2023: FLAP. DAMAGED. R/H WING INBD FLAP INNER SIDE NEAR MIDDLE SUPPORT HAS A SMALL HOLE "1/4 PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA OF MAIN FLAP PER SRM 51-70-06,PARAGRAPH 5. - [SDR FDEA202211302865](https://openairdocs.org/sdr/FDEA202211302865), Nov 30, 2022: BULB. INOPERATIVE. L1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1, REV 130.9, X1. - [SDR FDEA202211152785](https://openairdocs.org/sdr/FDEA202211152785), Nov 15, 2022: BEARING. MISALIGNED. AFTER LOADING, UNABLE TO LOCK MAIN CARGO DOOR, ONLY THE FWD CAM IS LOCKED, AFT CAM WOULD NOT MOVE. AMM: 52-32-00-5 DURING INSPECTION OF THE HOOK PIN, FOUND MISA - [SDR FDEA202206291618](https://openairdocs.org/sdr/FDEA202206291618), Jun 29, 2022: LAMP. INOPERATIVE. FOUND ARM/DISARM LIGHT SWITCH BULB INOP. RELAMPED ARM/DISARM LIGHT SWITCH FROM P82 PANEL AS PER AMM 33-30-00-0. OPN CHECK GOOD. OK FOR FURTHER SERVICE. - [SDR FDEA202203230764](https://openairdocs.org/sdr/FDEA202203230764), Mar 23, 2022: FLAP. DENTED. L/H WING OUTBD AFT FLAP FOUND SMALL DENT ON LOWER SURFACE CLOSE TO OUTBD END WITH ON DELAMINATION SIGHN PERFORMED WET LAYER REPAIR FOR MENTIONED AREA PER SRM 51 - [SDR FDEA202203210912](https://openairdocs.org/sdr/FDEA202203210912), Mar 21, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK UPPER FLANGE AT STA 880-860 AT RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5310-T0367599 CRACKED SEAT TRACK BTWN STA 860-880 LBL/RB - [SDR FDEA202203210911](https://openairdocs.org/sdr/FDEA202203210911), Mar 21, 2022: SEAT TRACK. NONE. FOUND MISSING PIECES OF UPPER FLANGE OF SEAT TRACK BETWEEN STA 880-860 AT LBL 45 WORK ACCOMPLISHED PER FEDEX E.A #F-5310-T0367599 CRACKED SEAT TRACK BTWN ST A86 - [SDR FDEA202202240930](https://openairdocs.org/sdr/FDEA202202240930), Feb 24, 2022: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOOR BEAM UPPER T-CHORD AT STA 880 BETWEEN RBL 45-68 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0367576 B, FLOOR BEAM ASSY , ST - [SDR FDEA202202240929](https://openairdocs.org/sdr/FDEA202202240929), Feb 24, 2022: FLOORBEAM. CORRODED. CORROSION WERE FOUND ON FLOOR BEAM UPPER T-CHORD LOCATED STA 880 LBL 45-60 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367576 B, FLOOR BEAM ASSY, - [SDR FDEA202202240834](https://openairdocs.org/sdr/FDEA202202240834), Feb 24, 2022: FLOORBEAM. CORRODED. CORRODED FLOOR BEAM UPPER T-CHORD LOCATED STA 1200 LBL 35-LBL 50 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367712: FLOOR BEAM AT STA 1200 BTWN L - [SDR FDEA202202240779](https://openairdocs.org/sdr/FDEA202202240779), Feb 24, 2022: SKIN. NONE. UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNAGE STA 1981.9-1941 11 O'CLOCK POSITION PERFORMED TAP TEST INSP. PER SRM 51-10-06 AND EVALUATED I.A.W CAS - [SDR FDEA202202240778](https://openairdocs.org/sdr/FDEA202202240778), Feb 24, 2022: SKIN. UNKNOWN. UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNSGE STA 1918.9-1941 12 O'CLOCK POSITION PERFORMED TAP TEST INSP PER SRM 51-10-06 AND EVALUATED I.A.W CASC - [SDR FDEA202202240767](https://openairdocs.org/sdr/FDEA202202240767), Feb 24, 2022: SKIN. DELAMINATED. FOUND CRACK AND DELAMINATION ON R/H WING LEADING EDGE SKIN UNDER SLAT #6 PERFORMED HOT BOND REPAIR FOR MENTIONED PANEL PER SRM 51-70-08, REF SRM 57-41-01- 2R, F - [SDR FDEA202202240766](https://openairdocs.org/sdr/FDEA202202240766), Feb 24, 2022: FLAP. NONE. UNDOCUMENTED COMPOSITE REPAIR ON L/H WING OUTER AFT FLAP LOWER SURFACE 11" FROM AFT EDGE 105" FROM OUTBD EDGE PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA PER - [SDR FDEA202202240763](https://openairdocs.org/sdr/FDEA202202240763), Feb 24, 2022: SKIN. UNKNOWN. UNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON STA 1963.8-1992.8 STR 6 O'CLOCK POSITION PERFORMED HOT BOND REPAIR PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R, DETAIL - [SDR FDEA202202240741](https://openairdocs.org/sdr/FDEA202202240741), Feb 24, 2022: SEAT TRACK. CORRODED. MULTIPE CORROSION WERE FOUND ON SEAT TRACK LOCATED STA 1180-1420 LBL 58 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367321. SEAT TRACK BTWN STA 1180-1420, LBL 58 - [SDR FDEA202202240740](https://openairdocs.org/sdr/FDEA202202240740), Feb 24, 2022: SEAT TRACK. CRACKED. CRACK ON SEAT TRACK LOCATED STA1580-1600 RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367320: SEAT TRACK AT STA 1580-1600 RBL 58.22, CRACK, PERMANENT REPAI - [SDR FDEA202202240708](https://openairdocs.org/sdr/FDEA202202240708), Feb 24, 2022: CHANNEL. UNKNOWN. UNDOCUMENTED REPAIR WERE FOUND ON 2 CHANNEL LOCATED STA 1380-1400 RBL 11 PERFORMED NEW SRM REPAIR PER SRM 53-60-52-2R, AND PER SRM 51-70-12 TYPICAL EXTRUDED REP - [SDR FDEA202202240707](https://openairdocs.org/sdr/FDEA202202240707), Feb 24, 2022: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LOCATED STA 1540 LBL 45.5 PERFORMED SEAT TRACK REPAIR USING NEW SEAT TRACK SECTION , 2 EA ANGLES, AND STRAP PER SRM 53-00-52, FIG 201, R - [SDR FDEA202202240642](https://openairdocs.org/sdr/FDEA202202240642), Feb 24, 2022: CHANNEL. UNKNOWN. UNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 RBL 29 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SR - [SDR FDEA202202240641](https://openairdocs.org/sdr/FDEA202202240641), Feb 24, 2022: CHANNEL. CORRODED. UNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 LBL 8 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM - [SDR FDEA202202240640](https://openairdocs.org/sdr/FDEA202202240640), Feb 24, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK UPPER CROWN AT STA 345-377 LBL 7 DAMAGED PART REMOVED AN NEW FABRICATED SEAT TRACK PER FEDEX EA # F-5310-T0367282 SUPERNUMERARY SE - [SDR FDEA202202240639](https://openairdocs.org/sdr/FDEA202202240639), Feb 24, 2022: NONE. NONE. MULTIPLE CORROSION ON SEAT TRACK BETWEEN STA 1280-1320 RBL 45 PERFORMED SEAT TRAK REPLACEMENT USING A NEW FABRICATED SEAT TRACK PER SRM 53- 00-52, FIG 201 REPAI - [SDR FDEA202202240611](https://openairdocs.org/sdr/FDEA202202240611), Feb 24, 2022: FLOORBEAM. CORRODED. CORROSION ON EXISTING REPAIR UPPER T-CHORD LOCATED STA 1540 LBL 10 PERFORMED REPAIR TO ONE FLANGE OF THE FLOOR BEAM UPPER CHORD PER SRM 53-00-51-2R, FIG.201, RE - [SDR FDEA202202220742](https://openairdocs.org/sdr/FDEA202202220742), Feb 22, 2022: BEAM. ELONGATED. FLOOR BEAM UPPER T CHORD STA 1681 FOUND WITH ELONGATED HOLE AT LBL 4 AND 2EA UNUSED HOLES AT RBL 12 PERFORMED AFT DECK AND FLOOR BEAM REPAIRS PER SRM 53-60-51-2 - [SDR FDEA202202220610](https://openairdocs.org/sdr/FDEA202202220610), Feb 22, 2022: SKIN. UNKNOWN. FOUND UNDOCUMENTED DOUBLER REPAIR AT DOOR 4R INNER SKIN ADJACENT TO STR 10R PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W EA F-5210-T0367359 AND NO DAMAGE - [SDR FDEA202202220609](https://openairdocs.org/sdr/FDEA202202220609), Feb 22, 2022: FLOORBEAM. UNKNOWN. FOUND UNDOCUMENTED UPPER T CHORD REPAIR AT STA 345 LBL 52-RBL52 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 53-00-51 AND MONARCH W/O 770838 NR AND NO - [SDR FDEA202202170381](https://openairdocs.org/sdr/FDEA202202170381), Feb 17, 2022: FLOOR PANEL. WORN. FLOOR PANEL P/N 11861182-16 AT STA 300 R/H FOUND WORN FABRICATED PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOCITION OF RFTA NO:02858-0204 P/N:N00236-T01-22 - [SDR FDEA202202170380](https://openairdocs.org/sdr/FDEA202202170380), Feb 17, 2022: FLOOR PANEL. WORN. FLOOR PANEL P.N 11861182-15 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204. P/N:N00236-T02-2 - [SDR FDEA202202170379](https://openairdocs.org/sdr/FDEA202202170379), Feb 17, 2022: FLOOR PANEL. WORN. FLOOR PANEL P/N 141N5361-213 AT STA 440 FOUND WORN FABRICATED THE PANEL IAW FEDEX SRZ-25-005, REF ENGINEERING DISPOSITION OF RFTA NO:02858-0204 P/N:N00236-T03-2 - [SDR FDEA202201300913](https://openairdocs.org/sdr/FDEA202201300913), Jan 30, 2022: SKIN. GOUGED. EVALUATE EXISTING REPAIR AT L/H WING O/B MAIN FLAP L/E PER EO F-5100-7-5001 PERFORMED DVI PER SRM 51-10-08 AND GOUGE FOUND ON EXISTING REPAIR. NEW REPAIR PERFOR - [SDR FDEA202110312703](https://openairdocs.org/sdr/FDEA202110312703), Oct 31, 2021: WARNING MESSAGE. FALSE ACTIVATION. ON FINAL AT 160-170 KNOTS, GOT RUDDER RATIO EICAS. HYDRAULIC PRESSURE WAS NORMAL. COMPLIED WITH QRH, AND DIVERTED DUE TO WIND LIMITATIONS. TROUBLELSHOOTING CARR - [SDR FDEA202107231845](https://openairdocs.org/sdr/FDEA202107231845), Jul 23, 2021: GIRT BAR. DIRTY. FORWARD ENTRY DOOR WILL NOT ARM. DOOR 1RH GIRT BAR MECHANISM INSPECTION PERFORMED I.A.W. AMM 52-11-25-5. FLOOR FITTINGS INSPECTED AND CLEANED. GIRT BAR RIPOSITI - [SDR FDEA202104230996](https://openairdocs.org/sdr/FDEA202104230996), Apr 23, 2021: SENSOR. DIRTY. RH DOOR SLIDE LIGHT INOP. DOOR 1R GIRT BAR PROXY SENSOR CLEANED. OPS TEST ACC AMM 25-66-11-2 REV 127.9 (SUBTASK 25-66-11-822-045 046) SATIS. DOOR 1R GIRT BAR PR All 184: https://openairdocs.org/aircraft/N913FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.